Aircraft crew exit hatch assemblies, systems, and methods. A crew exit path and a crew exit path exit in an aircraft wherein the crew exit path exit includes devices, systems, and methods for reliably deploying and retracting a support band within a positioned crew exit path hatch, wherein the crew exit path exit hatch is configured to be deployed within an aircraft passenger compartment in an aircraft.

    飞机机组人员离开舱口组件、系统和方法。飞机中的机组人员离开路径和机组人员离开路径出口,其中所述机组人员离开路径出口包括用于将支撑带可靠地部署和收起在所定位的机组人员离开路径出口舱口内的设备、系统和方法,其中机组人员离开路径出口舱口被配置为部署在飞机中的飞机乘客舱内。


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    Titel :

    Aircraft crew exit hatch assemblies, systems, and methods


    Weitere Titelangaben:

    飞机机组人员离开舱口组件、系统和方法


    Beteiligte:
    RENARD SCOTT E (Autor:in) / FARES JONATHAN (Autor:in) / FRECH ROBERT V (Autor:in) / KOLLER ANDREW P (Autor:in) / LEBLANC THOMAS L (Autor:in)

    Erscheinungsdatum :

    05.05.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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